• 한국기계가공학회지
• /
• 제20권12호
• /
• pp.24-29
• /
• 2021

Recently, owing to the high demand for eco-friendly cars in the automotive industry, noise and vibrations have become major challenges. The use of laminated damping steel is increasing in response to these demands. Laminated damping steel is primarily used in sound insulation plates. The vibration energy is converted into thermal energy due to the viscoelastic resin being located between two steel sheets and being able to damp the vibrations when an external force, such as, noise or vibration is applied to the steel plate. Laminated damping steel is chiefly applied to dash panels in automotive body parts, and because of its structure, junction technology for bonding with other components is necessary. However, there has not been sufficient research conducted on junctions. In this study, regardless of the electrode shape, in the range of 4.0 ~ 8.0 kA welding current, the same welding force and welding time were applied which were 2.8 kN and 200 m/s (12 cycles) and the tensile shear load and nugget size were analyzed after the resistance spot welding between different materials of laminated damping steel with a thickness of 1.035 mm. The results show that in the range of 5 ~ 8 kA welding current, 1.035 mm laminated damping steel meets the MS181-15 standard, which is the technical standard of Hyundai-Kia Motors.

• Coupled systems mechanics
• /
• 제11권5호
• /
• pp.439-458
• /
• 2022

Over-coating is one of the most popular engineering practices to strengthen Reinforced Concrete (RC) structures, due to the relative quickness and ease of construction. It consists of an external coat bonded to the outer surface of the structural RC element, either by the use of chemical adhesives, mechanical anchor bolts or simply mortar injection. In contrast to these constructive advantages, the numerical estimation of the bearing capacity of the strengthened reinforced concrete element is still complicated, not only for the complexity of modelling a flexible membrane or plate attached to a quasi-rigid solid, but also for the difficulties that raise of simulating any potential delamination between both materials. For these reasons, the standard engineering calculations used in the practice remain very approximated and clumsy. In this work, we propose the formulation of a new 2D solid-layer finite element capable to link a solid body with a flexible thin layer, as it were the "skin" of the body, allowing the potential delamination between both materials. In numerical terms, this "skin" element is intended to work as a transitional region between a solid body (modelled with a classical formulation of a standard quadrilateral four-nodes element) and a flexible coat layer (modelled with cubic beam element), dealing with the incompatibility of Degrees-Of-Freedom between them (two DOF for the solid and three DOF for the beam). The aim of the solid-layer element is to simplify the mesh construction of the strengthened RC element being aware of two aspects: a) to prevent the inappropriate use of very small solid elements to simulate the coat; b) to improve the numerical estimation of the real bearing capacity of the strengthened element when the coat is attached or detached from the solid body.

• 한국건축시공학회지
• /
• 제23권1호
• /
• pp.1-9
• /
• 2023

본 연구에서는 보편적으로 건물의 옥상 등에 사용되는 폴리 우레탄 방수재의 바탕구조물의 함수정도와 시공환경조건에 따른 하자원인을 분석하기 위한 것으로 바탕판의 함수조건에 따른 부착강도, 표면상태를 육안관찰하였고, 온도, 습도의 양생조건에 따라서 방수재 도막의 기계적 성능을 평가하였다. 실험결과 바탕판의 함수상태가 10%이상일 때 도막의 부착이 이뤄지지 않음을 확인하였고, 온습도 조건이 20℃, 80% RH일때는 기초물성이 모두 확보되었으나, 40℃, 60% RH일 때 표면에 기포가 관찰되었으며, 40℃, 80% RH일 때 건조도막 기초물성이 KS F 3211 성능기준이하로, 우레탄 방수재 도포에 있어 시공환경조건의 하자원인 중 바탕판의 함수조건 및 양생 시 절대습도가 중요한 요인임을 확인하였다.

• Coupled systems mechanics
• /
• 제12권6호
• /
• pp.481-501
• /
• 2023

Over-coating is one of the most popular engineering practices to strengthen Reinforced Concrete (RC) structures, due to the relative quickness and ease of construction. It consists of an external coat bonded to the outer surface of the structural RC element, either by the use of chemical adhesives, mechanical anchor bolts or simply mortar injection. In contrast to these constructive advantages, the numerical estimation of the bearing capacity of the strengthened reinforced concrete element is still complicated, not only for the complexity of modelling a flexible membrane or plate attached to a quasi-rigid solid, but also for the difficulties that raise of simulating any potential delamination between both materials. For these reasons, the standard engineering calculations used in the practice remain very approximated and clumsy. In this work, we propose the formulation of a new 2D solid-layer finite element capable to link a solid body with a flexible thin layer, as it were the "skin" of the body, allowing the potential delamination between both materials. In numerical terms, this "skin" element is intended to work as a transitional region between a solid body (modelled with a classical formulation of a standard quadrilateral four-nodes element) and a flexible coat layer (modelled with cubic beam element), dealing with the incompatibility of Degrees-OfFreedom between them (two DOF for the solid and three DOF for the beam). The aim of the solid-layer element is to simplify the mesh construction of the strengthened RC element being aware of two aspects: a) to prevent the inappropriate use of very small solid elements to simulate the coat; b) to improve the numerical estimation of the real bearing capacity of the strengthened element when the coat is attached or detached from the solid body.

• Restorative Dentistry and Endodontics
• /
• 제33권4호
• /
• pp.405-412
• /
• 2008

본 연구의 목적은 여러 가지 계면조건의 변화를 통해서 layering시 복합레진 층간의 결합에 oxygen inhibition layer (OIL)가 필수적인지를 고찰해보는 것이다. 가로 $\times$ 세로 $\times$ 두께가 16 $\times$ 28 $\times$ 2.5 mm인 알루미늄판에 지름 3.7 mm의 구멍을 형성하여 몰드를 제작하고 다음과 같이 복합레진 (Z-250, 3M ESPE)을 충전하여 광중합하였다. 1 군: 하층판에 복합레진을 충전하고 광중합 한 후, 상층판을 접합하고 레진을 충전하여 광중합을 하였다 (OIL를 남김). 2 군: 하층판에 복합레진을 충전하고 광중합 한 후 acetone에 적신 cotton으로 문질러서 OIL를 제거하고 상층판을 접합하여 복합레진을 충전하고 광중합을 하였다 (OIL를 제거). 3 군: 하층판에 복합레진을 충전하고 Mylar strip을 접합하여 공기와의 접촉을 차단한 후 광중합을 하였다. Mylar strip을 제거하고 상층판을 접합 후 복합레진을 충전하여 광중합을 하였다 (OIL형성을 억제). 4 군: 하층판에 복합레진을 충전하고 광중합 한 후 glycerin을 OIL 표면에 도포하고 다시 광중합하였다. 상층판을 접합하여 복합레진을 충전하고 광중합을 하였다 (OIL를 중합). 5군 (대조군): 하층판과 상층판의 경계에 복합레진층의 계면이 위치하지 않도록 복합레진을 bulk충전하였다 (계면형성 없이 bulk 충전한 복합레진). 24 시간 100% 습도에서 보관 후 상층판과 하층판 사이의 계면 전단결합강도를 측정하고 파절 양상을 관찰하였다. 계면을 통한 중합과정의 확산을 관찰하기 위하여 제조한 광개시제가 들어있지 않은 실험적 복합레진 (Exp_Com)을 몰드에 충전하고 상부에 flowable 복합 레진 (Aelite Flow) 또는 접착레진 (ScotchBond Multipurpose)을 접촉시킨 후 광조사하였다. 몰드내의 미중합된 Exp_Com을 acetone bath 에서 5 분 동안 제거한 후 몰드내에 다시 Aelite Flow를 충전하고 광중합을 시행하였다. 경화된 복합레진 시편의 단면을 관찰하여 Exp_Com 층의 두께를 측정하였다. OIL를 배제하거나 중합시킨 2-4군은 OIL이 존재하는 1 군과 통계적으로 유의한 결합강도의 차이를 보이지 않았으며, Mylar strip을 이용하여 OIL의 생성을 억제했던 3군과 glycerin을 도포하여 OIL를 중합시킨 4군은 계면을 생성하지 않은 대조군인 5 군과도 통계적으로 유의한 차이를 보이지 않았다. 중합과정의 확산에 의해 중합개시제가 포함되지 않은 Exp_Com내에 중합된 층이 생겨난 것을 시각적으로 확인할 수 있었으며, Exp_Com의 중합층 두께는 flowable 레진의 경우 20.95 (0.90) um였고 접착레진의 경우 42.13 (2.09) 였다.

• Journal of the Korean Wood Science and Technology
• /
• 제44권1호
• /
• pp.30-39
• /
• 2016

구조용 집성재 라멘 접합부에 일반적으로 사용되는 접합철물을 대신하여 단판과 Glass Fiber Reinforced Plastic (GFRP)를 복합시킨 GFRP 보강적층판과 삽입 접착형 GFRP rod를 접합물로 사용하여 낙엽송 집성재 문형라멘 구조의 수평가력 성능평가를 실시하였다. 실험결과 GFRP rod와 에폭시 접착제를 이용한 삽입 접착형 접합부는 기존의 접합철물을 이용한 실험체와 비교하여 항복내력, 종국내력, 초기강성이 각각 49%, 52%, 61% 낮게 측정되었다. 이러한 접합부는 GFRP rod와 집성재 간의 접착력이 중요한 내력 기구로 현장적용 시 문제가 발생할 수 있는 가능성이 크다고 판단된다. 반면, GFRP 보강적층판과 목재(Eucalyptus marginata)핀을 이용한 실험체는 집성재 슬릿 접합부의 단면적 손실이 큼에도 불구하고 항복내력, 종국내력, 초기강성, 소성률이 전부 3% 이내로 측정되었다. 게다가 사이클에 대한 강성변화율도 35%로 가장 낮게 측정되며 접합철물을 이용한 실험체와 거의 동등한 성능을 발휘한 것을 확인하였다.

• 콘크리트학회논문집
• /
• 제19권4호
• /
• pp.467-474
• /
• 2007

본 논문에서는 부착 유무, 정착장치 유무, 긴장량, 경간 길이 등을 실험 변수로 하여 총 13개의 시험체를 제작하여 휨 성능 실험과 유한요소해석을 수행하였다. 1개의 표준시험체, 2개의 긴장력을 도입하지 않는 보강시험체, 4개의 긴장력을 도입한 비부착보강시험체, 4개의 긴장력을 도입한 부착시험체와 2개의 경간 길이가 다른 보강시험체를 제작하였다. 또한, 콘크리트의 비선형, 철근 및 탄소섬유와 콘크리트와의 계면 특성을 고려한 DIANA 프로그램을 이용하여 비선형 유한요소해석을 수행하였다. 긴장력을 도입한 보강된 시험체는 박리 파괴가 아닌 FRP 파단에 의하여 최종파괴가 되었다. 특히, 긴장력을 도입한 부착시험체는 1차, 2차 박리가 발생 후, 정착장치의 고정으로 인하여 부착시스템에서 비부착시스템으로 전환되었다. 또한, 탄소섬유판으로 보강된 시험체의 해석 결과와 실험 결과를 비교 분석하였다. 긴장력을 도입한 탄소섬유판으로 보강된 모든 시험체는 연성지수가 3이상 나타나 어느 정도 이상의 연성을 확보하고 있는 것으로 알 수 있었다. 그리고 박리하중과 항복하중 및 극한하중에서 실험값과 해석값이 잘 일치하는 것으로 나타났다.

• 멤브레인
• /
• 제15권3호
• /
• pp.247-254
• /
• 2005

키토산 필름은 농업, 식품과 제약 분야에서 응용이 가능하다. 그러나 키토산으로만 만들어진 필름은 기체투과성이 높고 기계적 물성에 약하다. 따라서 본 연구에서는 기체 투과성을 낮추고 기계적 물성을 높이기 위해 층상구조를 갖는 점토광물의 일종인 montorillonite (MMT)와 양이온 생체고분자인 키토산을 이용하여 양이온 교환과 수소결합과정을 통해 $Na^+-MMT$에 키토산을 삽입하여 키토산/Clay 나노복합재료를 제조하였다. 키토산/clay 나노 복합재료의 X-ray 회절패턴에서 $2\theta=7.5^{\circ}$에서 MMT의 basal reflection이 나타났고, $2\theta=3\~5^{\circ}$ 주위에서의 새로운 약하고 넓은 peak로서 더 낮은 각에서 MMT의 basal reflection의 이동에 의해 삽입된 나노 구조의 형성을 증명하였다. 또한 TGA thermogram를 이용하여 clay의 함유량이 증가할수록 제조된 나노복합재료의 열분해가 일어나는 범위의 질량감소가 줄어드는 것을 확인하므로서 내열성을 관찰하였다. 기계적 물성 성질을 측정하여 clay 함유량의 증가에 따른 인장 강도와 인장 모듈러스의 변화를 관찰하고, 키토산이 층상 실리케이트 내에 삽입하여 제조된 나노복합재료에서 clay의 함유량이 증가할수록 질소 투과경로의 tortuosity를 증가시켜서 기체 투과도를 감소시키는 것도 확인하였다.

• 한국농공학회지
• /
• 제26권1호
• /
• pp.52-72
• /
• 1984

This study was performed to obtain the basic data which can be applied to the use of epoxy resin mortars. The data was based on the properties of epoxy resin mortars depending upon various mixing ratios to compare those of cement mortar. The resin which was used at this experiment was Epi-Bis type epoxy resin which is extensively being used as concrete structures. In the case of epoxy resin mortar, mixing ratios of resin to fine aggregate were 1: 2, 1: 4, 1: 6, 1: 8, 1:10, 1 :12 and 1:14, but the ratio of cement to fine aggregate in cement mortar was 1 : 2.5. The results obtained are summarized as follows; 1.When the mixing ratio was 1: 6, the highest density was 2.01 g/cm$^3$, being lower than 2.13 g/cm$^3$ of that of cement mortar. 2.According to the water absorption and water permeability test, the watertightness was shown very high at the mixing ratios of 1: 2, 1: 4 and 1: 6. But then the mixing ratio was less than 1 : 6, the watertightness considerably decreased. By this result, it was regarded that optimum mixing ratio of epoxy resin mortar for watertight structures should be richer mixing ratio than 1: 6. 3.The hardening shrinkage was large as the mixing ratio became leaner, but the values were remarkably small as compared with cement mortar. And the influence of dryness and moisture was exerted little at richer mixing ratio than 1: 6, but its effect was obvious at the lean mixing ratio, 1: 8, 1:10,1:12 and 1:14. It was confirmed that the optimum mixing ratio for concrete structures which would be influenced by the repeated dryness and moisture should be rich mixing ratio higher than 1: 6. 4.The compressive, bending and splitting tensile strenghs were observed very high, even the value at the mixing ratio of 1:14 was higher than that of cement mortar. It showed that epoxy resin mortar especially was to have high strength in bending and splitting tensile strength. Also, the initial strength within 24 hours gave rise to high value. Thus it was clear that epoxy resin was rapid hardening material. The multiple regression equations of strength were computed depending on a function of mixing ratios and curing times. 5.The elastic moduli derived from the compressive stress-strain curve were slightly smaller than the value of cement mortar, and the toughness of epoxy resin mortar was larger than that of cement mortar. 6.The impact resistance was strong compared with cement mortar at all mixing ratios. Especially, bending impact strength by the square pillar specimens was higher than the impact resistance of flat specimens or cylinderic specimens. 7.The Brinell hardness was relatively larger than that of cement mortar, but it gradually decreased with the decline of mixing ratio, and Brinell hardness at mixing ratio of 1 :14 was much the same as cement mortar. 8.The abrasion rate of epoxy resin mortar at all mixing ratio, when Losangeles abation testing machine revolved 500 times, was very low. Even mixing ratio of 1 :14 was no more than 31.41%, which was less than critical abrasion rate 40% of coarse aggregate for cement concrete. Consequently, the abrasion rate of epoxy resin mortar was superior to cement mortar, and the relation between abrasion rate and Brinell hardness was highly significant as exponential curve. 9.The highest bond strength of epoxy resin mortar was 12.9 kg/cm$^2$ at the mixing ratio of 1:2. The failure of bonded flat steel specimens occurred on the part of epoxy resin mortar at the mixing ratio of 1: 2 and 1: 4, and that of bonded cement concrete specimens was fond on the part of combained concrete at the mixing ratio of 1 : 2 ,1: 4 and 1: 6. It was confirmed that the optimum mixing ratio for bonding of steel plate, and of cement concrete should be rich mixing ratio above 1 : 4 and 1 : 6 respectively. 10.The variations of color tone by heating began to take place at about 60˚C, and the ultimate change occurred at 120˚C. The compressive, bending and splitting tensile strengths increased with rising temperature up to 80˚ C, but these rapidly decreased when temperature was above 800 C. Accordingly, it was evident that the resistance temperature of epoxy resin mortar was about 80˚C which was generally considered lower than that of the other concrete materials. But it is likely that there is no problem in epoxy resin mortar when used for unnecessary materials of high temperature resistance. The multiple regression equations of strength were computed depending on a function of mixing ratios and heating temperatures. 11.The susceptibility to chemical attack of cement mortar was easily affected by inorganic and organic acid. and that of epoxy resin mortar with mixing ratio of 1: 4 was of great resistance. On the other hand, when mixing ratio was lower than 1 : 8 epoxy resin mortar had very poor resistance, especially being poor resistant to organicacid. Therefore, for the structures requiring chemical resistance optimum mixing of epoxy resin mortar should be rich mixing ratio higher than 1: 4.

• 한국표면공학회:학술대회논문집
• /
• 한국표면공학회 2000년도 추계학술발표회 초록집
• /
• pp.3-4
• /
• 2000

Many researchers are interested in the synthesis and characterization of carbon nitride and diamond-like carbon (DLq because they show excellent mechanical properties such as low friction and high wear resistance and excellent electrical properties such as controllable electical resistivity and good field electron emission. We have deposited amorphous carbon nitride (a-C:N) thin films and DLC thin films by shielded arc ion plating (SAIP) and evaluated the structural and tribological properties. The application of appropriate negative bias on substrates is effective to increase the film hardness and wear resistance. This paper reports on the deposition and tribological OLC films in relation to the substrate bias voltage (Vs). films are compared with those of the OLC films. A high purity sintered graphite target was mounted on a cathode as a carbon source. Nitrogen or argon was introduced into a deposition chamber through each mass flow controller. After the initiation of an arc plasma at 60 A and 1 Pa, the target surface was heated and evaporated by the plasma. Carbon atoms and clusters evaporated from the target were ionized partially and reacted with activated nitrogen species, and a carbon nitride film was deposited onto a Si (100) substrate when we used nitrogen as a reactant gas. The surface of the growing film also reacted with activated nitrogen species. Carbon macropartic1es (0.1 -100 maicro-m) evaporated from the target at the same time were not ionized and did not react fully with nitrogen species. These macroparticles interfered with the formation of the carbon nitride film. Therefore we set a shielding plate made of stainless steel between the target and the substrate to trap the macropartic1es. This shielding method is very effective to prepare smooth a-CN films. We, therefore, call this method "shielded arc ion plating (SAIP)". For the deposition of DLC films we used argon instead of nitrogen. Films of about 150 nm in thickness were deposited onto Si substrates. Their structures, chemical compositions and chemical bonding states were analyzed by using X-ray diffraction, Raman spectroscopy, X-ray photoelectron spectroscopy and infrared spectroscopy. Hardness of the films was measured with a nanointender interfaced with an atomic force microscope (AFM). A Berkovich-type diamond tip whose radius was less than 100 nm was used for the measurement. A force-displacement curve of each film was measured at a peak load force of 250 maicro-N. Load, hold and unload times for each indentation were 2.5, 0 and 2.5 s, respectively. Hardness of each film was determined from five force-displacement curves. Wear resistance of the films was analyzed as follows. First, each film surface was scanned with the diamond tip at a constant load force of 20 maicro-N. The tip scanning was repeated 30 times in a 1 urn-square region with 512 lines at a scanning rate of 2 um/ s. After this tip-scanning, the film surface was observed in the AFM mode at a constant force of 5 maicro-N with the same Berkovich-type tip. The hardness of a-CN films was less dependent on Vs. The hardness of the film deposited at Vs=O V in a nitrogen plasma was about 10 GPa and almost similar to that of Si. It slightly increased to 12 - 15 GPa when a bias voltage of -100 - -500 V was applied to the substrate with showing its maximum at Vs=-300 V. The film deposited at Vs=O V was least wear resistant which was consistent with its lowest hardness. The biased films became more wear resistant. Particularly the film deposited at Vs=-300 V showed remarkable wear resistance. Its wear depth was too shallow to be measured with AFM. On the other hand, the DLC film, deposited at Vs=-l00 V in an argon plasma, whose hardness was 35 GPa was obviously worn under the same wear test conditions. The a-C:N films show higher wear resistance than DLC films and are useful for wear resistant coatings on various mechanical and electronic parts.nic parts.